View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66568U 26145.64790110 +.00000000 +00000-0 +93470-3 0 00006
2 66568 42.9984 272.0850 0001437 296.5354 63.5351 15.27600046 06
| Epoch (UTC): | 25 May 2026 15:32:58 |
| Eccentricity: | 0.0001437 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 272.0850° |
| argument of perigee: | 296.5354° |
| revolutions per day: | 15.27600046 |
| mean anomaly at epoch: | 63.5351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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